A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS REVISION 13 DEC 01/09

Transcription

1

2 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS REVISION 13 DEC 01/09 This revision concerns introduction of new pages and corrections of pages. Description of change. SECTION PAGE(s) REASON FOR CHANGE 1.1 p 1 Update Mail address. 1.2 p 1 and p 2 Update Presentation. 2.1 p 1 p 2 to p 2B Update Presentation. Update Presentation and added Weight Variants. 2.3 p 1 to p 2A Added Note on page 1 and Added Aircraft on Jack columns on pages 2 and 2A. 5.1 p 1 to p 3 Update Section. 5.2 p 1 Update Section. 5.3 p 1 Update Section p 11 Change 3/4 in. by Roylyn 1 in. 5.8 p 1 to p 6 Update Section and added new illustrations p 1 p 3 Added Illustration Danger Areas for PW4000 engines at Ground Idle. Added Illustration Acoustic Protection for PW4000 engines. 7.0 All pages Revised All Chapter. New Illustrations and New Text. 8.1 p 1 Change Text. 9.1 p 1 and p 2 Update Illustration. 9.2 p 1 and p 2 Update Illustration. HIGHLIGHTS Page 1 of 2 R DEC 01/09 Printed in France

3 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS REVISION 13 DEC 01/09 This revision concerns introduction of new pages and corrections of pages. Description of change. SECTION PAGE(s) REASON FOR CHANGE 9.3 p 1 and p 2 Delete Section. 9.4 p 1 and p 2 Delete Section. 9.5 p 1 and p 2 Delete Section. 9.6 p 1 and p 2 Delete Section. HIGHLIGHTS Page 2 of 2 R DEC 01/09 Printed in France

4 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING REVISION TRANSMITTAL SHEET TO : ALL HOLDERS OF A AIRPLANE CHARACTERISTICS R The revision, dated DEC 01/09 is attached and covers all the Airplane Characteristics, and the pavement data, which are identified in the highlights. FILING INSTRUCTIONS NOTE : Before introducing this revision make certain that previous revisions are incorporated. affected pages are listed on the List of Effective Pages and designated as follows : R = revised (to be replaced) D = deleted (to be removed) N = new (to be introduced). make certain that the content of the manual is in compliance with the List of Effective Pages. update the Record of Revisions page accordingly. file the Revision Transmittal Sheet separately. remove and destroy the pages which are affected by this revision. REASON FOR ISSUE The attached Highlights detail the reasons for issue. Page 1 of 1 R DEC 01/09 Printed in France

5 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING RECORD OF REVISIONS REV No. ISSUE DATE DATE INSERTED BY REV No. ISSUE DATE DATE INSERTED BY R FEB 28/83 1 MAR 31/83 2 APR 30/83 3 FEB 29/84 4 OCT 01/87 5 FEB 01/88 6 AUG 31/88 7 OCT 31/89 8 OCT 31/90 9 JUN 30/92 10 MAR 31/93 11 OCT 30/94 12 JUN 01/98 13 DEC 01/09 RECORD OF REVISIONS Page 1 R DEC 01/09 Printed in France

6 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING LIST OF EFFECTIVE PAGES CHAPTER/ PAGE DATE CHAPTER/ PAGE DATE SECTION SECTION L.E.P. R 1 DEC 09 L.E.P. R 2 DEC 09 L.E.P. R 3 DEC 09 R.O.R. R 1 DEC 09 T.O.C. R 1 DEC 09 T.O.C. R 2 DEC 09 T.O.C. R 3 DEC 09 T.O.C. D 4 DEC 09 T.O.C. D 5 DEC 09 T.O.C. D 6 DEC R 1 DEC R 1 DEC R 1 DEC R 2 DEC R 1 DEC R 1 DEC R 2 DEC R 2A DEC N 2B DEC MAR OCT OCT OCT OCT R 1 DEC R 2 DEC N 2A DEC FEB A JUN B JUN FEB FEB JUN FEB FEB FEB FEB FEB FEB FEB FEB FEB FEB OCT FEB FEB FEB FEB OCT OCT FEB OCT OCT OCT OCT OCT OCT OCT FEB FEB FEB FEB AUG AUG FEB FEB FEB FEB FEB R 1 DEC R 1 DEC R 2 DEC R 3 DEC D 4 DEC D 5 DEC D 6 DEC D 7 DEC D 8 DEC D 9 DEC 09 LIST OF EFFECTIVE PAGES Page 1 R DEC 01/09 Printed in France

7 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING LIST OF EFFECTIVE PAGES CHAPTER/ PAGE DATE CHAPTER/ PAGE DATE SECTION SECTION 5.2 R 1 DEC D 2 DEC D 3 DEC R 1 DEC FEB FEB FEB FEB JUN FEB OCT FEB OCT BLANK R 11 DEC OCT FEB FEB FEB APR APR APR R 1 DEC R 2 DEC N 3 DEC N 4 DEC N 5 DEC N 6 DEC R 1 DEC OCT OCT OCT OCT JUN OCT OCT JUN OCT OCT AUG OCT OCT AUG OCT OCT AUG OCT OCT AUG OCT OCT OCT OCT OCT N 3 DEC OCT OCT AUG OCT JUN N 3 DEC OCT R 1 DEC R 1 DEC R 2 DEC R 3 DEC N 4 DEC R 1 DEC N 2 DEC N 3 DEC R 1 DEC R 1 DEC D 2 DEC N 1 DEC N 2 DEC N 3 DEC R 1 DEC D 2 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC R 1 DEC 09 LIST OF EFFECTIVE PAGES Page 2 R DEC 01/09 Printed in France

8 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING LIST OF EFFECTIVE PAGES CHAPTER/ PAGE DATE CHAPTER/ PAGE DATE SECTION SECTION 7.6 D 2 DEC D 3 DEC D 4 DEC D 5 DEC D 6 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC R 1 DEC D 2 DEC D 3 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC R 1 DEC D 2 DEC D 3 DEC D 7 DEC D 5 DEC D 6 DEC D 7 DEC D 8 DEC N 1 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC N 1 DEC N 1 DEC R 1 DEC D 2 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC D 1 DEC D 2 DEC D 3 DEC N 1 DEC N 2 DEC N 3 DEC N 4 DEC N 5 DEC D 1 DEC D 2 DEC D 3 DEC D 1 DEC D 2 DEC R 1 DEC R 1 DEC R 1 DEC R 1 DEC R 2 DEC R 1 DEC R 2 DEC D 1 DEC D 2 DEC D 1 DEC D 2 DEC D 1 DEC D 2 DEC D 1 DEC D 2 DEC 09 LIST OF EFFECTIVE PAGES Page 3 R DEC 01/09 Printed in France

9 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING TABLE OF CONTENTS R R R R R R 1.0 SCOPE 1.1 Purpose 1.2 Introduction 2.0 AIRPLANE DESCRIPTION 2.1 General Airplane Characteristics 2.2 General Airplane Dimensions 2.2 Airplane Dimensions Airplane Dimensions PW Engines Airplane Dimensions GE Engines CF6 80C2 2.3 Ground Clearances 2.4 Interior Arrangements Passengers Cargo (14 Pallets) Cargo (13 Pallets) Cargo (Mixed Pallets : 9 + 5) 2.5 Passenger Compartment Cross Section Seating Configuration.6 Abreast.First Class Seating Configuration.8 Abreast.all tourist Class Seating Configuration.9 Abreast.High Density Version 2.6 Lower Compartments Containers Pallets In Forward Cargo Compartment 2.7 Door Clearances Forward Passenger/Crew Door Mid Passenger/Crew Door Emergency Exit Aft Passenger/Crew Door Forward Cargo Compartment Aft Cargo Compartment Door Bulk Cargo Compartment Door Upper Deck Cargo Door Radome Travel 3.0 AIRPLANE PERFORMANCE 3.1 General Information 3.2 Payload Range Payload Range Long Range Cruise (PW JT9D 7R4H1) Payload Range Long Range Cruise (GE CF6 80C2) 3.3 Far Take off Runway Length requirements CONTENTS Page 1 R DEC 01/09 Printed in France

10 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING TABLE OF CONTENTS ISA Conditions ISA + 15 C Conditions 3.4 FAR Landing Runway Lenght Requirements All Ambient Temperatures 3.5 Landing Approach Speed Landing Approach Speed At 1.3 Vs 4.1 Minimum Turning Radii Main Landing Gears With Original Bogie Main Landing Gears With La Guardia Bogie 4.4 Visibility From Compartment in Static Position 4.5 Runway and Taxiway Turn Paths More than 90 Deg. Turn To Taxiway Turn Deg. Turn Runway to Taxiway Deg. Turn Taxiway to Taxiway 4.6 Runway Holding Bay (Apron) R R R R R R 5.0 TERMINAL SERVICING 5.1 Airplane Servicing Arrangements Symbols Used On Servicing Diagrams 5.2 Terminal Operations Turnaround Station 5.3 Terminal Operations En Route Station 5.4 Ground Service Connections Symbols Used On Ground Service Connections Diagrams Ground Service Connections Hydraulic System Electrical System Oxygen System Fuel System Pneumatic System Potable Water System Toilet System Vacuum Toilet System 5.5 Engine Starting Pneumatic Requirements Ambient Temperature 40 C ( 40 F) Ambient Temperature +15 C (+60 F) Ambient Temperature C (+100 F) 5.6 Ground Pneumatic Power Requirements Heating Cooling 5.7 Preconditioned Airflow Requirements 5.8 Ground Towing Requirements CONTENTS Page 2 R DEC 01/09 Printed in France

11 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING TABLE OF CONTENTS R R R R R R N R N R N R N R N N R N N N R R R R 6.0 OPERATING CONDITIONS 6.1 Jet Engine Exhaust Velocities And Temperatures Exhaust Velocity Contours Breakaway Power Exhaust Temperature Contours Breakaway Power Exhaust Velocity Contours Take off Power Exhaust Temperature Contours Take off Power Exhaust Velocity Contours Idle Power Exhaust Temperature Contours Idle Power 6.2 Airport and Community Noise Noise Data 6.3 Danger Areas of the Engines Danger Areas of the Engines Ground Idle Danger Areas of the Engines Take off Accoustic Protection Areas APU Exhaust GAS Temperature and Velocity DECAY APU 7.0 PAVEMENT DATA 7.1 General Information 7.2 Landing Gear Footprint 7.3 Maximum Pavement Loads Models 7.4 LG Loading on Pavement LG Loading on Pavement 7.5 Flexible Pavement Requirements U.S. Army Flexible Pavement Requirements 7.6 Flexible Pavement Requirements LCN Flexible Pavement Requirements LCN 7.7 Rigid Pavement Requirements PCA Rigid Pavement Requirements PCA 7.8 Rigid Pavement Requirements LCN Radius of Relatives Stiffness Inches Rigid Pavement Requirements LCN 7.9 ACN PCN Reporting System ACN Number Flexible Pavement ACN Number Rigid Pavement 8.0 DERIVATIVE AIRPLANES 8.1 Possible Future A Derivative Airplanes 9.0 SCALED DRAWINGS 9.1 Scaled Drawing 1 in. = 500 ft. 9.2 Scaled Drawing 1 cm. = 500 cm. CONTENTS Page 3 R DEC 01/09 Printed in France

12 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 1.0 SCOPE R R 1.1 Purpose 1.2 Introduction Chapter 1.0 Page 1 R DEC 01/09 Printed in France

13 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 1.1 Purpose The A AIRPLANE CHARACTERISTICS (AC) manual is issued for the A basic versions to provide the necessary data needed by airport operators and airlines for the planning of airport facilities. This document conforms to NAS CORRESPONDENCE Correspondence concerning this publication should be directed to : AIRBUS S.A.S. Customer Services Technical Data Support and Services 1, Rond Point Maurice BELLONTE BLAGNAC CEDEX FRANCE Chapter 1.1 Page 1 R DEC 01/09 Printed in France

14 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 1.2 Introduction This manual comprises 9 chapters with a List of Effective Pages (LEP) and a Table Of Content (TOC) at the beginning of each chapter. Chapter 1 : SCOPE Chapter 2 : AIRPLANE DESCRIPTION This chapter contains general dimensional and other basic aircraft data. It covers : aircraft dimensions and ground clearances, passengers and cargo compartments arrangement. Chapter 3 : AIRPLANE PERFORMANCE This chapter indicates the aircraft performance. It covers : payload range, takeoff and landing runway requirements, landing approach speed. Chapter 4 : GROUND MANEUVERING This chapter provides the aircraft turning capability and maneuvering characteristics on the ground. It includes : turning radii and visibility from the cockpit, runway and taxiway turn path. Chapter 5 : TERMINAL SERVICING This chapter provides information for the arrangement of ground handling and servicing equipments. It covers : location and connections of ground servicing equipments, engines starting pneumatic and preconditioned airflow requirements. Chapter 1.2 Page 1 R DEC 01/09 Printed in France

15 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Chapter 6 : OPERATING CONDITIONS This chapter contains data and safety/environmental precautions related to engine and APU operation on the ground. It covers : contour size and shape of the jet engine exhaust velocities and temperature, noise data. Chapter 7 : PAVEMENT DATA This chapter contains the pavement data helpful for airport planning. It gives : landing gear foot print and static load, charts for flexible pavements with Load Classification Number (LCN), charts for rigid pavements with LCN, Aircraft Classification Number (ACN), Pavement Classification Number (PCN), reporting system for flexible and rigid pavements. Chapter 8 : DERIVATIVE AIRPLANES This chapter gives relevant data of possible new version with the associated size change. Chapter 9 : SCALED DRAWING This chapter contains different A scaled drawings. Chapter 1.2 Page 2 R DEC 01/09 Printed in France

16 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2.0 AIRPLANE DESCRIPTION R R 2.1 General Airplane Characteristics 2.2 General Airplane Dimensions 2.3 Ground Clearances 2.4 Interior Arrangements 2.5 Passenger Compartment Cross Section 2.6 Lower Compartment 2.7 Door Clearances Chapter 2.0 Page 1 R DEC 01/09 Printed in France

17 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2.1 General Airplane Characteristics The weight terms used throughout this manual are given below together with their respective definitions. Maximum Taxi Weight (MTW) : Maximum weight for ground maneuver as limited by aircraft strength and airworthiness requirements. (It includes weight of run-up and taxi fuel). It is also called Maximum Ramp Weight (MRW). Maximum Landing Weight (MLW) : Maximum weight for landing as limited by aircraft strength and airworthiness requirements. Maximum Takeoff Weight (MTOW) : Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This is the maximum weight at start of the takeoff run). Maximum Zero Fuel Weight (MZFW) : Maximum operational weight of the aircraft without usable fuel. Operational Empty Weight (OEW) : Weight of structure, powerplant, furnishings, systems, and other items of equipment that are an integral part of a particular aircraft configuration plus the operator s items. The operator s items are the flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toilet chemical and fluids, galley structure, catering equipment, passenger seats and life vests, documents, etc. Maximum Payload : Maximum Zero Fuel Weight (MZFW) minus Operational Empty Weight (OEW). Maximum Seating Capacity : Maximum number of passengers specifically certified or anticipated for certification. Maximum Cargo Volume : Maximum usable volume available for cargo. Usable Fuel : Fuel available for aircraft propulsion. Chapter 2.1 Page 1 R DEC 01/09 Printed in France

18 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING AIRPLANE VERSION A300B4 600 A300C4 600 PAX A300C4 600 FREIGHT WV000 (Basic) WV008 WV000 (Basic) WV000 (Basic) Maximum Taxi kg Weight (MTW) lb Maximum Takeoff kg Weight (MTOW) lb Maximum Landing kg Weight (MLW) lb Maximum Zero Fuel kg Weight (MZFW) lb GE CF kg ( lb) Engines Estimated PW4000 Operational Empty kg ( lb) Engines Weight (OEW) PW JT9D kg kg kg ( lb) Engines ( lb) ( lb) Estimated kg Maximum Payload GE CF6 80 lb Estimated kg Maximum Payload PW4000 lb Estimated kg Maximum Payload PW JT9D lb Standard Seating Single Capacity class Usable l (2) Fuel US Gallons (2) Capacity kg (d=0.785) (2) lb (2) Pressurized m Fuselage Volume (A/C non equipped) ft Passenger m Compartment Volume ft Cockpit m Volume ft Usuable Cargo m Compartment Volume (1) ft (1) Volume of Cargo Compartments : Fwd Cargo Compartment : m3 (2 702 ft3) Aft Cargo Hold Compartment : m3 (2 155 ft3) Bulk Cargo Compartment : 21 m3 (742 ft3) (2) ACT only for WV000 with PW JT9D engine General Airplane Characteristics Data Chapter 2.1 Page 2 R DEC 01/09 Printed in France

19 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING AIRPLANE VERSION A300B4 600R WV000 (Basic) WV001 WV002 WV003 Maximum Taxi kg Weight (MTW) lb Maximum Takeoff kg Weight (MTOW) lb Maximum Landing kg Weight (MLW) lb Maximum Zero Fuel kg Weight (MZFW) lb Estimated Operational Empty Weight (OEW) Estimated Maximum Payload Estimated Maximum Payload Standard Seating Capacity GE CF6 80 Engines kg ( lb) PW4000 Engines kg ( lb) kg GE CF6 80 lb kg PW4000 lb single class Usable l Fuel US Gallons Capacity kg (d=0.785) lb Pressurized m3 860 Fuselage Volume (A/C non equipped) ft Passenger m3 574 Compartment Volume ft Cockpit m3 12 Volume ft3 424 Usuable Cargo m Compartment Volume (1) ft (1) Volume of Cargo Compartments : Fwd Cargo Compartment : m3 (2 702 ft3) Aft Cargo Hold Compartment : m3 (2 155 ft3) Bulk Cargo Compartment : 21 m3 (742 ft3) 274 General Airplane Characteristics Data Chapter 2.1 Page 2A R DEC 01/09 Printed in France

20 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING AIRPLANE VERSION A300B4 600R WV004 WV005 WV007 WV008 WV010 Maximum Taxi kg Weight (MTW) lb Maximum Takeoff kg Weight (MTOW) lb Maximum Landing kg Weight (MLW) lb Maximum Zero Fuel kg Weight (MZFW) lb Estimated Operational Empty Weight (OEW) Estimated Maximum Payload Estimated Maximum Payload Standard Seating Capacity GE CF6 80 Engines kg ( lb) PW4000 Engines kg ( lb) kg GE CF6 80 lb kg PW4000 lb single 274 class Usable l Fuel US Gallons Capacity kg (d=0.785) lb Pressurized m3 860 Fuselage Volume (A/C non equipped) ft Passenger m3 574 Compartment Volume ft Cockpit m3 12 Volume ft3 424 Usuable Cargo m Compartment Volume (1) ft (1) Volume of Cargo Compartments : Fwd Cargo Compartment : m3 (2 702 ft3) Aft Cargo Hold Compartment : m3 (2 155 ft3) Bulk Cargo Compartment : 21 m3 (742 ft3) General Airplane Characteristics Data Chapter 2.1 Page 2B N DEC 01/09 Printed in France

21

22

23

24

25

26 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2.3 Ground Clearances NOTE : The distances given in the Ground Clearances charts are reference distances calculated for A/C weight and CG conditions. The conditions used in the calculations are maximum A/C weight (minimum ground clearances) and a typical A/C maintenance weight (typical ground clearances for maintenance). Chapter 2.3 Page 1 R DEC 01/09 Printed in France

27 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2.3 Ground Clearances Chapter 2.3 Page 2 R DEC 01/09 Printed in France

28 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2.3 Ground Clearances Chapter 2.3 Page 2A N DEC 01/09 Printed in France

29

30

31

32

33

34

35

36

37

38

39

40

41

42

43

44

45

46

47

48

49

50

51

52

53

54

55

56

57

58

59

60

61

62

63

64

65

66

67

68

69

70

71 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING R R R R R 5.0 TERMINAL SERVICING 5.1 Airplane Servicing Arrangements 5.2 Terminal Operations Turnaround Station 5.3 Terminal Operations En Route Station 5.4 Ground Service Connections 5.5 Engine Starting Pneumatic Requirements 5.6 Ground Pneumatic Power Requirements 5.7 Preconditioned Airflow Requirements 5.8 Ground Towing Requirements Chapter 5.0 Page 1 R DEC 01/09 Printed in France

72 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING This section provides typical ramp layouts, showing the various GSE items in position during typical turnaround scenarios. These ramp layouts show typical arrangements only. Each operator will have its own specific requirements/regulations for the positioning and operation on the ramp. For each ramp layout, the associated typical turnaround time is given in a Chart in section 5.2 for the passenger aircraft and section 5.3 for the cargo aircraft. AS AIR STARTING VEHICLE BC BULK CONVEYOR BF BULK FREIGHT VEHICLE C CABIN CLEANING TRUCK CPL CONTAINER/PALLET LOADER CPT CONTAINER/PALLET TRANSPORTER CS CABIN CLEANERS STEPS F REFUELING VEHICLE FC FREIGHT/CARGO TRAIN G GALLEY LOADING VEHICLE GC PRECONDITIONED AIR GROUND TRUCK GPU ELECTRICAL GROUND POWER UNIT MDL MAIN DECK LOADER PS PASSENGER ACCESS STEPS T TOILET SERVICING VEHICLE W WATER REPLENISHMENT VEHICLE Airplane Servicing Arrangements Symbols Used On Servicing Diagrams Model A A300C4 600 Chapter 5.1 Page 1 R DEC 01/09 Printed in France

73 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Airplane Servicing Arrangements Typical Open Apron Free Standing Model A Chapter 5.1 Page 2 R DEC 01/09 Printed in France

74 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Airplane Servicing Arrangements Typical Open Apron Free Standing Model A300C4 600 Chapter 5.1 Page 3 R DEC 01/09 Printed in France

75 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 5.2 Terminal Operations Turnaround Station This section provides a chart showing typical activities for intermediate turnaround. This data is provided to show the general scope and type of activities involved in ramp operations during the turnaround of an aircraft. Varying Airline practices and operating circumstances may result in different sequences and different time intervals to do the activities shown. Terminal Operations Turnaround Station Model A Chapter 5.2 Page 1 R DEC 01/09 Printed in France

76 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 5.3 Terminal Operations En Route Station This section provides a chart showing typical activities for home base turnaround. This data is provided to show the general scope and type of activities involved in ramp operations during the turnaround of an aircraft. Varying Airline practices and operating circumstances may result in different sequences and different time intervals to do the activities shown. Terminal Operations En Route Station Model A300C4 600 Chapter 5.3 Page 1 R DEC 01/09 Printed in France

77

78

79

80

81

82

83

84

85

86

87 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING TOILET SYSTEM DISTANCE : Meters (ft) AFT OF NOSE FROM AIRPLANE CENTERLINE RH SIDE LH SIDE MEAN HEIGHT FROM GROUND R R Per servicing panel One standard 4 in. drain connection and one Roylyn 1 in. in front and two Roylyn 1 in. flush connection behind (14-5) (143-7) 0.64 (2-1) 1.71 (5-7) 3.29 (10-9) 4.29 (14.0) Capacity Single toilet : Waste : 58.7 liters (12.9 Imp. gal) (15.5 US gal) Chemical fluid : 9.5 liters ( 2.1 Imp. gal) ( 2.5 US gal) Capacity Double toilet : Waste : 120 liters (26.4 Imp. gal) (31.6 US gal) Chemical fluid : 19 liters ( 4.2 Imp. gal) ( 5.0 US gal) Ground Service Connections Toilet System Model A Chapter Page 11 R DEC 01/09 Printed in France

88

89

90

91

92

93

94

95 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 5 8 Ground Towing Requirements This section provides information on aircraft Towing. The A is designed with means for conventional towing or towbarless towing. Information on towbar less towing can be found in SIL and chapter 9 of the Aircraft Maintenance Manual. 1. Ground Towing It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idle thrust, using a towbar attached to the nose gear leg. Two towbar fittings are installed, one at the front of the leg and one at the back. The body gears have attachment points for towing or debogging (for details refer to chapter 7 of the Aircraft Recovery Manual). A. The first part of this section shows the chart to determine the draw bar pull and tow tractor mass requirements as function of the following physical characteristics : Aircraft weight Slope Number of engines at idle The chart is based on the A engine type with the biggest idle thrust. The chart is therefore valid for all A models. B. The second part of this section supplies guidelines for the towbar. NOTE : Information on aircraft towing procedures and corresponding aircraft limitations are given in chapter 9 of the Aircraft Maintenance Manual. Ground Towing Requirements Chapter 5.8 Page 1 R DEC 01/09 Printed in France

96 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Ground Towing Requirements Chapter 5.8 Page 2 R DEC 01/09 Printed in France

97 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 2. Towbar design guidelines The aircraft towbar shall respect the following norms : SAE AS 1614, Main Line Aircraft Tow Bar Attach Fitting Interface, SAE ARP1915 Revision C, Aircraft Tow Bar, ISO , Aircraft Tow bar attachment fitting Interface requirements Part 1 : Main line aircraft, ISO 9667, Aircraft ground support equipment Tow bars IATA Airport Handling Manual AHM 958, Functional Specification for an Aircraft Towbar A conventional type tow bar is required which should be equipped with a damping system to protect the nose gear against jerks and with towing shear pins : A traction shear pin calibrated at dan (36500 lbf), A torsion pin calibrated at 1750 m.dan (12907 lbf.in). The towing head is designed according to SAE/AS 1614 (issue C) cat. II. There is a variety of shear pin arrangements and the values of the shear pins depend on them. We hereafter show two arrangements classically used on towbars. Ground Towing Requirements Chapter 5.8 Page 3 N DEC 01/09 Printed in France

98 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Ground Towing Requirements Typical Tow Bar Configuration 1 Chapter 5.8 Page 4 N DEC 01/09 Printed in France

99 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Ground Towing Requirements Typical Tow Bar Configuration 2 Chapter 5.8 Page 5 N DEC 01/09 Printed in France

100 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Ground Towing Requirements Nose Gear Towing Fittings Chapter 5.8 Page 6 N DEC 01/09 Printed in France

101 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING R R 6.0 OPERATING CONDITIONS 6.1 Jet Engine Exhaust Velocities and Temperatures Exhaust Velocity Contours Breakaway Power Exhaust Temperature Contours Breakaway Power Exhaust Velocity Contours Take off Power Exhaust Temperature Contours Take off Power Exhaust Velocity Contours Idle Power Exhaust Temperature Contours Idle Power 6.2 Airport and Community Noise Noise Data 6.3 Danger Areas of the Engines Danger Areas of the Engines Ground Idle Danger Areas of the Engines Take off Acoustic Protection Areas APU Exhaust Gas Temperature and Velocity DECAY APU Definition of Breakaway Power Breakaway Power means the minimum power necessary for the aircraft to be able to start moving. Chapter 6.0 Page 1 R DEC 01/09 Printed in France

102

103

104

105

106

107

108

109

110

111

112

113

114

115

116

117

118

119

120

121

122

123

124

125

126

127 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 6.3 Danger Areas of the Engines Danger Areas of the Engines Ground Idle (PW4000 Engine) Chapter Page 3 N DEC 01/09 Printed in France

128

129

130

131

132

133 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 6.3 Danger Areas of the Engines Danger Areas of the Engines Acoustic Protection (PW4000 Engine) Chapter Page 3 N DEC 01/09 Printed in France

134

135 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.0 PAVEMENT DATA 7.1 General Information 7.2 Landing Gear Footprint 7.3 Maximum Pavement Loads 7.4 LG Loading on Pavement LG Loading on Pavement 7.5 Flexible Pavement Requirements U.S. Army Flexible Pavement Requirements 7.6 Flexible Pavement Requirements LCN Flexible Pavement Requirements LCN 7.7 Rigid Pavement Requirements PCA Rigid Pavement Requirements PCA 7.8 Rigid Pavement Requirements LCN Radius of Relatives Stiffness Inches Rigid Pavement Requirements LCN Radius of Relative Stiffness Other values Radius of Relative Stiffness Other values 7.9 ACN PCN Reporting System ACN Number Flexible Pavement ACN Number Rigid Pavement Chapter 7.0 Page 1 R DEC 01/09 Printed in France

136 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.1 General Information A300B4 600 Models 1. General Information PAVEMENT DATA A brief description of the pavement charts that follow will help in airport planning. To aid in the interpolation between the discrete values shown, each airplane configuration is shown with a minimum range of five loads on the main landing gear. All curves on the charts represent data at a constant specified tire pressure with : the airplane loaded to the maximum ramp weight. the CG at its maximum permissible aft position. Pavement requirements for commercial airplanes are derived from the static analysis of loads imposed on the main landing gear struts. Section 7.2.0, presents basic data on the landing gear footprint configuration, maximum ramp weights and tire sizes and pressures. Section 7.3.0, shows maximum vertical and horizontal pavement loads for certain critical conditions at the tire ground interfaces. Section contains charts to find these loads throughout the stability limits of the airplane at rest on the pavement. These main landing gear loads are used as the point of entry to the pavement design charts which follow, interpolating load values where necessary. Section uses procedures in Instruction Report No. S 77 1 Procedures for Development of CBR Design Curves, dated June 1977 to show flexible pavement design curves. The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station, Soils and Pavement Laboratory, Vicksburg, Mississippi. Section & uses the new load repetition factor according to the ICAO letter Reference AN 4/20.1-EB/07/26. Chapter 7.1 Page 1 R DEC 01/09 Printed in France

137 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING The line showing coverages is used to calculate Aircraft Classification Number (ACN). 2. Flexible Pavement The procedure that follows is used to develop flexible pavement design curves such as shown in Section A. With the scale for pavement thickness at the bottom and the scale for CBR at the top, an arbitary line is drawn representing coverages. B. Incremental values of the weight on the main landing gear are then plotted. C. Annual departure line are drawn based on the load lines of the weight on the main landing gear that is shown on the graph. Section gives the rigid pavement design curves that have been prepared with the use of the Westergaard Equation. This is in general accordance with the procedures outlined in the Portland Cement Association publications, Design of Concrete Airport Pavement, 1973 and Computer Program for Airport Pavement Design, (Program PDILB), 1967 both by Robert G. Packard. 3. Rigid Pavement The procedure that follows is used to develop rigid pavement design curves such a those shown in Section A. With the scale for pavement thickness on the left and the scale for allowable working stress on the right, an arbitrary line load line is drawn. This represents the main landing gear maximum weight to be shown. B. All values of the subgrade modulus (k values) are then plotted. C. Additional load lines for the incremental values of weight on the main landing gear are drawn on the basis of the curve for k = 80 MN/m 3 already shown on the graph. All Load Classification Number (LCN) curves shown in Section and Section have been developed from a computer program based on data provided in Internation Civil Aviation Organisation (ICAO) document 7920 AN/865/2, Aerodrome Manual, Part 2, Aerodrome Physical Characteristics, Second Edition, Chapter 7.1 Page 2 R DEC 01/09 Printed in France

138 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING The flexible pavement charts in Section show LCN against equivalent single wheel load, and equivalent single wheel load against pavement thickness. The rigid pavement charts in Section show LCN against equivalent single wheel load, and equivalent single wheel load against radius of relative stiffness. Section provides ACN data prepared according to the ACN/PCN system as referenced in ICAO Annex 14, Aerodromes, Volume 1 Aerodrome Design and Operations. Fourth Edition July 2004, incorporating Amendments 1 to 6. The ACN/PCN system provides a standardized international airplane/pavement rating system replacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world. ACN is the Aircraft Classification Number and PCN is the corresponding Pavement Classification Number. An aircraft having an ACN equal to or less than the PCN can operate without restriction on the pavement. Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms. The derived single wheel load is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) that would have the same pavement requirements as the aircraft. Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S 77 1 for flexible pavements to calculate ACN values. The Airport Authority must decide on the method of pavement analysis and the results of their evaluation shown as follows : PCN PAVEMENT TYPE R Rigid F Flexible SUBGRADE CATEGORY A High B Medium C Low D Ultra Low TIRE PRESSURE CATEGORY W No Limit X To 1.5 Mpa (217 psi) Y To 1 Mpa (145 psi) Z To 0.5 Mpa (73 psi) EVALUATION METHOD T Technical U Using Aircraft Chapter 7.1 Page 3 R DEC 01/09 Printed in France

139 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Section shows the aircraft ACN values for flexible pavements. The four subgrade categories are : A High Strength CBR 15 B Medium Strength CBR 10 C Low Strength CBR 6 D Ultra Low Strength CBR 3 Section shows the aircraft ACN for rigid pavements. The four subgrade categories are : A High Strength Subgrade k = 150 MN/m 3 (550 pci) B Medium Strength Subgrade k = 80 MN/m 3 (300 pci) C Low Strength Subgrade k = 40 MN/m 3 (150 pci) D Ultra Low Strength Subgrade k = 20 MN/m 3 (75 pci) Chapter 7.1 Page 4 N DEC 01/09 Printed in France

140 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Footprint A300B4 600 Models MRW kg Chapter 7.2 Page 1 R DEC 01/09 Printed in France

141 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Footprint A300B4 600R Models MRW kg Chapter 7.2 Page 2 N DEC 01/09 Printed in France

142 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Footprint A300B4 600R Models MRW kg Chapter 7.2 Page 3 N DEC 01/09 Printed in France

143 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Maximum Pavement Loads Chapter 7.3 Page 1 R DEC 01/09 Printed in France

144 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.4 Landing Gear Loading on Pavement A300B4 600 Models In the typical example shown in Section 7.4.1, with MRW kg. The Gross Aircraft Weight is kg ( lb) and the percentage of weight on the Main Gear is 95 %. For these conditions the total weight on the Main Gear Group is kg ( lb). Chapter 7.4 Page 1 R DEC 01/09 Printed in France

145 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Loading on Pavement A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

146 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Loading on Pavement A300B4 600R Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

147 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Landing Gear Loading on Pavement A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

148 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.5 Flexible Pavement Requirements US Army Corps of Engineers Design Method To find a Flexible Pavement Thickness, the Subgrade Strength (CBR), the Annual Departure Level and the weight on one Main Landing must be known. A300B4 600 Models In the typical example shown in Section with MRW kg for : a CBR value of 10 an Annual Departure level of 3000 and the load on one Wing Landing Gear of kg ( lb) the required Flexible Pavement Thickness is 39 cm (16 inches). The line showing Coverages is used to calculate Aircraft Classification Number (ACN). Chapter 7.5 Page 1 R DEC 01/09 Printed in France

149 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

150 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

151 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

152 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

153 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

154 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.6 Flexible Pavement Requirements LCN Conversion A300B4 600 Models To find the airplane weight that a Flexible Pavement can support, the LCN of the pavement and the thickness (h) must be known. In the example shown in Section with MRW kg. The thickness (h) is shown at 762 mm (30 in.) with an LCN of 96. For these conditions the weight on one Main Landing Gear is kg ( lb). Chapter 7.6 Page 1 R DEC 01/09 Printed in France

155 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements LCN A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

156 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements LCN A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

157 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

158 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

159 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Flexible Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

160 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.7 Rigid Pavement Requirements Portland Cement Association Design Method A300B4 600 Models To determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable working stress and the weight on one Main Landing Gear must be known. In the typical example shown in Section with MRW kg for : a k value of 80 MN/m 3 (K = 300 lbf/in 3 ) an allowable working stress of 28 kg/cm 2 (400 lb/in 2 ) the Load on one Wing Landing Gear of kg ( lb) the required Rigid Pavement Thickness is 28 cm (11 inches). Chapter 7.7 Page 1 R DEC 01/09 Printed in France

161 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

162 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

163 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

164 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

165 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

166 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.8 Rigid Pavement Requirements LCN Conversion A300B4 600 Models To determine the airplane weight that a Rigid Pavement can support, the LCN of the pavement and the Radius of Relative Stiffness (L) must be known. In the typical example shown in Section with MRW kg. The Radius of Relative Stiffness is shown at 1143 mm (45 in.) with an LCN of 86. For these conditions the weight on one Main Landing Gear is kg ( lb). Chapter 7.8 Page 1 R DEC 01/09 Printed in France

167 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Radius of relative stiffness (Reference : Portland Ciment Association) Chapter Page 1 N DEC 01/09 Printed in France

168 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements LCN A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

169 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements LCN A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

170 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

171 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

172 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Rigid Pavement Requirements LCN A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

173 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Radius of Relative Stiffness (Other values of E and μ) A300B4 600 Models The table Radius of Relative Stiffness of Chapter presents L values based on Young s Modulus (E) of psi and Poisson s Ratio (μ) of To find L values based on other values of E and μ, See Section Radius of Relative Stiffness. For example, to find an L value based on an E of psi, the E factor of is multiplied by the L value found in the table Radius of Relative Stiffness of Section The effect of variations of μ on the L value is treated in a similar manner. Chapter Page 1 N DEC 01/09 Printed in France

174 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Radius of relative stiffness (Effect E and μ on L values) Chapter Page 1 N DEC 01/09 Printed in France

175 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 7.9 ACN/PCN Reporting System A300B4 600 Models To find the ACN of an aircraft on flexible or rigid pavement, the aircraft gross weight and the subgrade strength must be known. In the example shown in Section 7.9.1, with MRW kg. For an Aircraft Gross Weight of kg ( lb) and low subgrade strength (code B), the ACN for the flexible pavement is 35. In the example shown in Section 7.9.2, with MRW kg. For an Aircraft Gross Weight kg ( lb) and low subgrade strength (code B), the ACN for the rigid pavement is 37. NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on that pavement, subject to any limitation on the tire pressure. (Ref. ICAO Aerodrome Design Manual Part 3 Chapter 1 Second Edition 1983). Chapter 7.9 Page 1 R DEC 01/09 Printed in France

176 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Flexible Pavement A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

177 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Flexible Pavement A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

178 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Flexible Pavement A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

179 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Flexible Pavement A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

180 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Flexible Pavement A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

181 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Rigid Pavement A300B4 600 Models MRW kg Chapter Page 1 N DEC 01/09 Printed in France

182 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Rigid Pavement A300B4 600 Models MRW kg Chapter Page 2 N DEC 01/09 Printed in France

183 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Rigid Pavement A300B4 600R Models MRW kg Chapter Page 3 N DEC 01/09 Printed in France

184 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Rigid Pavement A300B4 600R Models MRW kg Chapter Page 4 N DEC 01/09 Printed in France

185 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING Aircraft Classification Number Rigid Pavement A300B4 600R Models MRW kg Chapter Page 5 N DEC 01/09 Printed in France

186 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING R 8.0 DERIVATIVE AIRPLANES 8.1 Possible Future A Derivative Airplane Chapter 8.0 Page 1 R DEC 01/09 Printed in France

187 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING R 8.1 Possible Future A Derivative Airplane No more derivatives are planned for A Chapter 8.1 Page 1 R DEC 01/09 Printed in France

188 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING R R 9.0 SCALED DRAWINGS 9.1 A Scaled Drawing 1 in. = 500 ft. 9.2 A Scaled Drawing 1 cm. = 500 cm. Chapter 9.0 Page 1 R DEC 01/09 Printed in France

189 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 9.1 Scaled Drawing 1 in. = 500 ft. Chapter Page 1 R DEC 01/09 Printed in France

190 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 9.1 Scaled Drawing 1 in. = 500 ft. Chapter Page 2 R DEC 01/09 Printed in France

191 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 9.2 Scaled Drawing 1 cm. = 500 cm. Chapter Page 1 R DEC 01/09 Printed in France

192 A AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING 9.2 Scaled Drawing 1 cm. = 500 cm. Chapter Page 2 R DEC 01/09 Printed in France